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ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 2 OF 15
Form 0230-001a Rev 3
PART LIST
ITEM QTY PART NUMBER DESCRIPTION REMARKS
NOT REQUIRED
TOOL LIST ITEM QTY PART NUMBER DESCRIPTION REMARKS
1 1 USN52L ULTRASONIC EQUIPMENT
2 1 HS225‐5‐70 SEARCH UNIT
3 1 HS225‐5‐60 SEARCH UNIT
4 1 HS225‐5‐65 SEARCH UNIT
5 1 99D57103017000 REFERENCE BLOCK
6 1 99D57103018000 REFERENCE BLOCK
7 1 99D57103019000 REFERENCE BLOCK
8 1 L1CM74‐2 CABLE
9 1 ZG5 Couplant or equivalent
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 3 OF 15
Form 0230-001a Rev 3
REVISION RECORD
N° REVISION ITEM DESCRIPTION DATE
0
ALL
ORIGINAL RELEASE
August 28, 2012 (LG)
1
TOOL LIST
Tool list updated. Reference block P/N
99D57103020000 was replaced by Reference block P/N
99D57103017000
November 20, 2013 (LG)
SKY FLEET
CONFIGURATION
Sky fleet configuration and applicability updated
2
ALL
COMPLETE REVISION DUE SB A320-57-1130 UPDATING TO REV. 3
CONFIGURATION DEFINITION
UPDATED
DELETED A/C CC-ADP; CC-ADO
ADDED A/C CC-AFY AND CC-AHC
August 10, 2016 (LG)
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
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Aug-10-2016
2 4 OF 15
Form 0230-001a Rev 3
TABLE 1 CONFIGURATION DEFINITION
CONF 001
Config. 001 is valid for A319-100 aircraft model.
CONF 002 Config. 002 is valid for A320-200 aircraft model.
CONF 003
Config. 003 is valid for A318-100 aircraft model. SKY FLEET CONFIGURATION:
AIRCRAFT CONFIG. PER S/B 57‐1130
Rev. 3 Compliance Time
(whichever occurs first) Repetitive interval
(whichever occurs first)
CC‐ABW; MSN 1523 002 48000 FC /96000 FH from Entry Into Service (EIS)
7600FC / 15200FH CC‐ABV; MSN 1400 002
CC‐AFY; MSN 2129 001 48000 FC /96000 FH from Entry Into Service (EIS)
9100FC /18300FH CC‐AHC; MSN 2119 001
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 5 OF 15
Form 0230-001a Rev 3
TABLE 2
SKY FLEET CONFIGURATION AND APPLICABILITY:
AIRCRAFT APPLICABILITY
CC‐ABW; MSN 1523 YES
CC‐ABV; MSN 1400 YES
CC‐AFY; MSN 2129 YES
CC‐AHC; MSN 2119 YES
CC‐AFX; MSN 2283 NO
CC‐AFZ; MSN 2251 NO
CC‐AHD; MSN 2460 NO
CC‐AHE; MSN 2548 NO
CC‐AIB; MSN 2378 NO
CC‐AIC; MSN 2380 NO
CC‐AID; MSN 2436 NO
CC‐AIY; MSN 2214 NO
CC‐AJF; MSN 2249 NO
CC‐AMP; MSN 3171 NO
CC‐AJG; MSN 3331 NO AIRBUS A319 series aircraft, all certified models, all serial numbers (MSN), except aircraft that have received: - AIRBUS modifications (mod) 28238, 28162 and 28342 in production, or - mod 33421 in production. AIRBUS A320 series aircraft, all certified models, all serial numbers (MSN), except aircraft that have received mod 33421 fully embodied in production. Note: AIRBUS A320 aircraft that have partially received mod 33421 in production are affected by the requirements of this E.O.
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 6 OF 15
Form 0230-001a Rev 3
GENERAL
WARNING:
MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION:
ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO THIS:
— PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC;
AS NECESSARY ON WIRING AND COMPONENTS.
— REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 7 OF 15
Form 0230-001a Rev 3
TASK DESCRIPTION MEC LICENSE
& SIGNATURE
INSPECTOR &
SIGNATURE
ACCOMPLISHMENT INSTRUCTIONS
Config. 001
Task 571130-832-801-001 – Inspection
PREPARATION :
Subtask 571130-941-002-001 - Job Set-up General
A. Make sure that the aircraft is grounded, refer to AMM Task 12-34-24-869-
002
M I
Subtask 571130-941-004-001 - Job Set-up on RH Side
A. Put the access platforms in position at zone 640.
M
B. Remove the panels 192LB and 148DB on the wing to fuselage, refer to
AMM Task 53-35-11-000-001.
M
Subtask 571130-941-005-001 - Job Set-up on LH Side
C. Put the access platforms in position at zone 540.
M
D. Remove the panels 191LB and 147CB on the wing to fuselage, refer to
AMM Task 53-35-11-000-001.
M
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 8 OF 15
Form 0230-001a Rev 3
TASK DESCRIPTION MEC LICENSE
& SIGNATURE
INSPECTOR &
SIGNATURE
PROCEDURE
Subtask 571130-832-004-001 - Do an External Ultrasonic Inspection of the lower panels in the center and outer wing box at level of RIB 1 junction (RH Side)
A. Clean the inspection areas with solvent Non Aqueous Cleaner-General.
M I
B. Do an external ultrasonic inspection of the lower panels in the center
and outer wing box at level of Rib 1 junction, as specified in NTM 57-11-75, refer to Figure A-FBAAA and Figure A-FFAAA
CRACK FOUND ON RH SIDE YES NO If crack is found contact Engineering Department before next flight and follow their instructions. If crack is not found, follow with the next steps
I
Subtask 571130-832-005-001 - Do an External Ultrasonic Inspection of the lower panels in the center and outer wing box at level of RIB 1 junction (LH Side)
A. Do an external ultrasonic inspection of the lower panels in the center
and outer wing box at level of Rib 1 junction, as specified in NTM 57-11-75, refer to Figure A-FBAAA and Figure A-FFAAA
CRACK FOUND ON LH SIDE YES NO If crack is found contact Engineering Department before next flight and follow their instructions. If crack is not found, follow with the next steps
I
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 9 OF 15
Form 0230-001a Rev 3
TASK DESCRIPTION MEC LICENSE
& SIGNATURE
INSPECTOR &
SIGNATURE
CLOSE UP
Subtask 571130-942-004-001 - Close-up on RH Side
A. Make sure that the work areas are clean and clear of tools and other
items of equipment.
M I
B. Install the panels 192LB and 148DB on the wing to fuselage, refer to
AMM Task 53-35-11-400-001
M I
C. Remove the access platform(s).
M I
Subtask 571130-942-005-001- Close-up on LH Side
A. Make sure that the work areas are clean and clear of tools and other
items of equipment.
M I
B. Install the panels 191LB and 147CB on the wing to fuselage, refer to
AMM Task 53-35-11-400-001
M I
C. Remove the access platform(s).
M I
Subtask 571130-942-006-001 - Close-up General
A. Put the aircraft back to its initial configuration.
M
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 10 OF 15
Form 0230-001a Rev 3
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 11 OF 15
Form 0230-001a Rev 3
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 12 OF 15
Form 0230-001a Rev 3
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 13 OF 15
Form 0230-001a Rev 3
ENGINEERING ORDER N° A319/A320-57/1319
Engineering Management Pudahuel, Santiago, Chile
WORK ORDER :
ITEM NUMBER :
DATE:
REV:
PAGE:
Aug-10-2016
2 14 OF 15
Form 0230-001a Rev 3
Deviation Record Sheet Paragraph Observation Action Authorized by Performed by